As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BORE CORRODED RIGHT WING INBOARD FLAP OUTBOARD HINGE LOWER SWIVEL BEARING. REMOVED CORROSION IAW DACCMM 57-44-07. ORIGINAL BORE 2.530 INCH FINAL 2.543 INCH MATERIAL LOSS .013 INCH. FABBED BUSHING IAW DACCMM 57-44-07 AND EA8-5750-81474. PERFORMED MPI IAW DPS 4.704. CAD PLATED BUSHING IAW DACCMM 57-44-07. ALODINED AND PRIMED BORE IAW DC10 SRM 51-201 VOLUME II. INSTALLED AND HONED BUSHING IAW DACCMM 57-44-07.